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Article

Highly Accurate Attitude Estimation of Unmanned Aerial Vehicle Payloads Using Low-Cost MEMS

1
School of Aerospace Science and Technology, Xidian University, Xi’an 710071, China
2
CCTEG Xi’an Research Institute (Group) Co., Ltd., Xi’an 710077, China
3
Qian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, China
4
365th Research Institute, Northwestern Polytechnical University, Xi’an 710072, China
*
Author to whom correspondence should be addressed.
Micromachines 2025, 16(6), 632; https://doi.org/10.3390/mi16060632
Submission received: 23 April 2025 / Revised: 20 May 2025 / Accepted: 27 May 2025 / Published: 27 May 2025
(This article belongs to the Special Issue MEMS Inertial Device, 2nd Edition)

Abstract

Low-cost MEMS sensors are widely utilized in UAV platforms to address attitude estimation problems due to their compact size, low power consumption, and cost-effectiveness. Diverse UAV payloads pose new challenges for attitude estimation, such as magnetic interference environments and high dynamic environments. In this paper, we propose a hierarchical decoupled attitude estimation algorithm, termed HDAEA. Initially, a novel hierarchical decoupling approach is introduced for the attitude and angle representation of the direction cosine matrix, enabling the representation of angles in a new manner. This method reduces the data dimensionality and nonlinearity of observation equations. Furthermore, a magnetic interference identification algorithm is proposed to compute the magnetic interference intensity accurately and quantitatively. Combining the quantified errors of estimated state variables, an error model for magnetic interference and attitude angles in high-dynamic environments is constructed. Subsequently, the proposed error model is employed to calibrate the hierarchical decoupled angles using accelerometer and magnetometer measurements, effectively mitigating the impact of magnetic interference on the calculation of pitch angles and roll angles. Moreover, the integration of the proposed hierarchical decoupled attitude estimation algorithm with the error-state extended Kalman filter reduces system nonlinearity and minimizes linearization errors. Experimental results demonstrate that HDAEA exhibits significantly improved attitude estimation accuracy of UAV payloads.
Keywords: MEMS; error-state extended Kalman filter (ESKF); magnetic interference; orientation decoupling; attitude estimation; multifunctional payloads MEMS; error-state extended Kalman filter (ESKF); magnetic interference; orientation decoupling; attitude estimation; multifunctional payloads

Share and Cite

MDPI and ACS Style

Zhou, X.; Chen, L.; Sun, C.; Jia, W.; Yi, N.; Sun, W. Highly Accurate Attitude Estimation of Unmanned Aerial Vehicle Payloads Using Low-Cost MEMS. Micromachines 2025, 16, 632. https://doi.org/10.3390/mi16060632

AMA Style

Zhou X, Chen L, Sun C, Jia W, Yi N, Sun W. Highly Accurate Attitude Estimation of Unmanned Aerial Vehicle Payloads Using Low-Cost MEMS. Micromachines. 2025; 16(6):632. https://doi.org/10.3390/mi16060632

Chicago/Turabian Style

Zhou, Xuyang, Long Chen, Changhao Sun, Wei Jia, Naixin Yi, and Wei Sun. 2025. "Highly Accurate Attitude Estimation of Unmanned Aerial Vehicle Payloads Using Low-Cost MEMS" Micromachines 16, no. 6: 632. https://doi.org/10.3390/mi16060632

APA Style

Zhou, X., Chen, L., Sun, C., Jia, W., Yi, N., & Sun, W. (2025). Highly Accurate Attitude Estimation of Unmanned Aerial Vehicle Payloads Using Low-Cost MEMS. Micromachines, 16(6), 632. https://doi.org/10.3390/mi16060632

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